4.7 Article

Analysis of Space-Borne GPS Data Quality and Evaluation of Precise Orbit Determination for COSMIC-2 Mission Based on Reduced Dynamic Method

Journal

REMOTE SENSING
Volume 14, Issue 15, Pages -

Publisher

MDPI
DOI: 10.3390/rs14153544

Keywords

COSMIC-2; space-borne GPS; quality assessment; reduced dynamic method; precise orbit determination

Funding

  1. National Natural Science Foundation of China [41704015, 41774001]
  2. Shandong Natural Science Foundation of China [ZR2017MD032, ZR2021MD030]
  3. Project of Shandong Province Higher Education Science and Technology Program [J17KA077]
  4. Talent introduction plan for Youth Innovation Team in universities of Shandong Province (innovation team of satellite positioning and navigation)

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COSMIC-2 is a remote sensing satellite mission that provides scientific data for weather forecasting, ionosphere, and climate research. The study evaluated the quality of space-borne GPS observation data and achieved precise orbit determination for COSMIC-2 using the reduced dynamic method. The results showed low data utilization, frequent cycle slips, and interruptions in carrier-phase data.
COSMIC-2 is a remote sensing satellite mission that mainly provides scientific data for weather forecasting, ionosphere, and climate research. High precise orbit is the basis for the application of remote sensing satellite data. In order to realize the precise orbit determination (POD) of COSMIC-2, we have assessed the quality of space-borne GPS observation in detail, including the utilization of GPS observations, cycle slip ratio (o/slps), multipath error, single-noise ratio (SNR) and ionospheric delay rate (IOD) of the data, realized the POD of COSMIC-2 with the reduced dynamic (RD) method, and evaluated the accuracy of the solved orbit by means of the carrier-phase residual, overlapping orbit comparison and the reference orbit comparison. The data quality assessments show that the data is less affected by the multipath effect, the utilization of the data is low, cycle slips occur frequently, and the carrier-phase data is often interrupted. The POD results indicate that the root mean square (RMS) values of the carrier-phase residuals of six COSMIC-2 satellites are between 6.0 mm and 7.5 mm, The mean RMS values of the overlapping orbit are better than 0.92 cm, 1.33 cm and 1.03 cm in the radial (R), tangential (T) and normal (N) directions respectively, and the mean RMS values of the six satellites in the 3D direction are between 1.38 cm and 1.75 cm. The mean RMS values in R, T and N directions orbit determination accuracy of the reference orbit comparison are better than 5.61 cm, 6.59 cm and 2.29 cm respectively, and the mean RMS values of the six satellites in the 3D direction are between 7.35 cm and 8.79 cm.

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